高续航力无人机电动混合动力系统的评价

B. Gang, Keun-Bae Kim
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摘要

本研究展示了用于高续航无人机的6千瓦级混合动力系统的测试性能。动力系统由二冲程往复发动机、起动发电机和蓄电池组成,并集成为一个动力单元。发动机被设计成在曲轴末端提供容纳起动-发电机的房子,使发动机和起动-发电机在运行期间能保持相同的转速。通过这种方式,产生的功率很容易通过操纵发动机节气门运动来控制。此外,起动发电机可以在电池的帮助下启动发动机运行,直到燃烧过程变得稳定。因此,简化了发动机与发电机之间的集成机制,从而实现了重量的减轻。备用电池的作用是通过系统控制器为发电机提供启动电源,以弥补暂时的电力短缺。因此,通过地面试验,电力系统可以提供6kw的功率。
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The Evaluation of an Electric Hybrid Power System for the High Endurance Drone
This research shows the test performance of a 6 kW-scale hybrid electric power system for the high endurance drone. The power system is composed of a two-stroke reciprocal engine, starter-generator and battery, and they are integrated as one power unit. The engine is designed to provide the house for holding the starter-generator at the end of a crankshaft in turn the engine and starter-generator can maintain the same speed during the operational period. In this way, the generated power is readily controlled by just manipulating an engine throttle movement. Moreover, the starter-generator can initiate an engine operation with an aid of battery power until the combustion process becomes stabilized. In consequence, integration mechanism between an engine and generator is simplified, which results in weight reduction achieved. The duty of back-up battery is to provide a starting power to generator via a system controller in addition to covering momentarily power shortage. Therefore, the electric power system is vindicated to provide 6 kW power through a ground test.
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